Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 3741
This examiner grants 75% of resolved cases
Marc J Amar examines cases in Tech Center 3700 and Art Unit 3741. The examiner has 413 resolved cases with an allowance rate of 75.1 percent. This 75.1 percent rate shows a strong probability of success for applicants, with a majority of cases reaching a grant. The median days to allowance is 1118, which serves as a benchmark for the duration of successful prosecution.
The interview lift is significant at 37.8 percent. This 37.8 percent lift suggests that interviews are a highly effective tool for overcoming rejections, even with a high base allowance rate of 75.1 percent. Practitioners should prioritize interviews to navigate the 1118-day median prosecution period and resolve any technical or legal disagreements. The 413 resolved cases indicate a well-established pattern of examination that favors direct communication. This data suggests that while the examiner is generally inclined to grant, an interview can substantially accelerate or secure that outcome.
| App # | Title | Status | Assignee |
|---|---|---|---|
| 17991101 | METHOD FOR MANAGING THE AMOUNTS OF POWER DRAWN FROM POWER UNITS OF THE PROPULSION UNITS OF AN AIRCRAFT | Final Rejection | Airbus Operations (S.A.S.) |
| 18129640 | POWER COUPLING BETWEEN ENGINE ROTATING ASSEMBLY AND EXTERNAL DEVICE | Non-Final OA | Pratt & Whitney Canada Corp. |
| 18575953 | ADMINISTRATION OF NAKED NUCLEIC ACID MOLECULE | Non-Final OA | Daicel Corporation |
| 18675233 | PROPULSION SYSTEM ARCHITECTURE | Non-Final OA | General Electric Company |
| 18089635 | METHODS AND APPARATUS FOR HEATING AND TEMPERATURE MONITORING | Final Rejection | ASM IP Holding B.V. |
| 18372836 | METHOD OF OPERATING A GAS TURBINE ENGINE | Final Rejection | ROLLS-ROYCE plc |
| 18838442 | EXHAUST NOZZLE | Non-Final OA | BAE SYSTEMS plc |
| 18594479 | Aircraft Thrust Reverser Corrosion Shield | Final Rejection | Textron Aviation Inc. |
| 18340341 | METHOD TO DECREASE ACOUSTIC SIGNATURE OF A HYBRID ELECTRIC PROPULSION SYSTEM | Final Rejection | RTX Corporation |
| 17586326 | HYBRID ELECTRIC SINGLE ENGINE DESCENT RESTART | Final Rejection | RTX Corporation |
| 18580075 | GAS SEALED ACCESS CAP FOR A ROBOTIC CANNULA AND METHOD OF PERFORMING A ROBOTICALLY ASSISTED SURGICAL PROCEDURE | Non-Final OA | Conmed Corporation |
| 18149884 | COOKING APPLIANCE AND METHODS OF NOTIFICATION | Non-Final OA | Haier US Appliance Solutions, Inc. |
| 18202709 | THRUST VECTORING EXHAUST NOZZLE FOR AIRCRAFT PROPULSION SYSTEM | Non-Final OA | Raytheon Technologies Corporation |
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